[IGSREPORT-16123] Wk 1472 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Apr 10 06:15:22 PDT 2008
******************************************************************************
IGS Electronic Report 10 Apr 06:15:42 PDT 2008 Message Number 16123
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1472 (Mar 23, 2008 - Mar 29, 2008)
Contact: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the centers
absolute deviation to the unweighted average orbit after removing small
differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.1472.
For long arc computations the Earth Orientation Parameters (EOPs) are fixed to
the values of the final IGS (GPS) combination.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
Weber R., 2000, IGS Technical Report 1999
PRODUCTS GENERATED:
-------------------
The combined IGL-ephemerides are written to daily files in the SP3-format.
The satellite accuracy codes in the header are based on the weighted rms.
for each satellite. Note, that the result files contain all satellites
that were analysed by at least one center. We refer to the 'REMARKS' section
below, in case a satellite or center was excluded from the combination.
The following naming convention is used for the result files:
igl1472[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1472 in the SP3 format.
igl14727.sum Combination Report for GPS Week 1472.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only.
3. Starting on 01-May-2005 (GPS Week 1321; MJD 53491)[IGSMAIL-5151]
BKG, ESA, and CODE will start to refer their GLONASS orbit products
to the following satellite antenna offset (SAO) values:
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets derived from the
bkg summary files were added to the broadcast clocks.
Day | applied clock offset
----+---------------------
0 | 1204.6 ns
1 | 1186.5 ns
2 | 1136.8 ns
3 | 1161.8 ns
4 | 1157.9 ns
5 | 1092.8 ns
6 | 1110.1 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
1 | ESX | R04
2 | ESX | R11
4 | ESX | R01
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.1472, 1a.1472).
Table 2 contains the complete ephemeris and clock correction transformation
parameters (includes both the apriori and a posteriori values) for each
centre and each day (Tables 2.1472.0-6)
Table 3 contains two types of daily RMS for each satellite and centre, along
with the computed satellite position sigmas for the combined orbits
(tables 3.1472.0-6).
The first type of satellite RMS is based on orbit combination and the
second RMS type is a result of the 7-day arc evaluation of each centre
ephemerides.
Table 1: Week 1472 summary. (Mar 23, 2008 - Mar 29, 2008)
Table 1.1472.a GPS week : 1472 MJD: 54548.0-54554.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 67| 2 -1 -3 -47 30 -105 -.13 40 37 | 0 49 2568 2659
| 3 1 3 26 36 185 .04 | 0 242
cod 175| 0 1 -1 39 8 59 -.17 26 22 | --- --- --- ---
| 1 1 4 21 41 64 .05 | --- ---
esx 113| 1 -2 -3 -4 -49 2 .35 99 58 | -5855 2058 7446 22672
| 5 4 7 43 68 98 .22 | 27230 5793
iac n/a| 1 0 4 -25 12 -24 .18 53 53 | 1149413 -2091 7318 15650
| 3 2 8 37 58 56 .06 | 37969 3445
mcc n/a| -5 2 31 -20 84 1188 .17 283 283 | --- --- --- ---
| 13 18 36 326 210 1242 .83 | --- ---
Table 1.1472.b GPS week : 1472 MJD: 54548.0-54554.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R01 | 17 16 23 19 16 23 15 |
R04 | 14 15 22 14 11 19 16 |
R06 | 17 16 19 23 24 20 14 |
R07 | 15 16 16 20 18 22 15 |
R08 | 29 41 31 39 25 34 36 |
R09 | 43 16 35 30 22 12 22 |
R10 | 19 18 17 21 29 18 24 |
R11 | 23 28 42 39 29 16 27 |
R13 | 19 30 22 24 21 44 27 |
R14 | 11 16 18 13 15 20 15 |
R15 | 18 27 23 31 33 20 19 |
R17 | 48 28 31 27 29 29 26 |
R19 | 29 37 36 34 27 17 17 |
R20 | 24 29 29 29 22 24 18 |
R23 | 34 23 25 32 37 30 36 |
R24 | 19 19 19 20 21 24 19 |
Table 1.1472.c GPS week : 1472 MJD: 54548.0-54554.0
Daily transformation of broadcast orbits (brd) to the combined IGL orbit.
Mean and standard deviations of the transformation parameters for the
whole gpsweek.
CEN WEEK DAY | DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm] | [ps] [ps/d]
-------------+------------------------------------------------------------+----------------
brd 1472 0 | 54 -72 475 3722 1512 -15350 93.4 5946 5946 | 1204580 0
brd 1472 1 | 131 -123 20860 -1329 2745 -23750 102.1 >>>>> >>>>> | 1186461 0
brd 1472 2 | -17 -95 552 -435 -1384 -21430 92.2 4575 4575 | 1136812 0
brd 1472 3 | 78 -40 500 -8 3358 -20030 92.7 4850 4850 | 1161795 0
brd 1472 4 | 85 226 429 173 1865 -20810 94.6 6559 6559 | 1157891 0
brd 1472 5 | -208 -204 124 6383 4806 -21550 98.0 6579 6579 | 1092800 0
brd 1472 6 | -180 110 384 -2335 -5 -29140 92.9 6876 6876 | 1110059 0
-------------+------------------------------------------------------------+----------------
brd 1472 mean| -7 -28 3332 881 1842 -21722 95.1 >>>>> >>>>> | 1150056 0
brd 1472 sdev| 135 147 7730 3071 2074 4154 3.6 >>>>> >>>>> | 39897 0
Table 2: Daily transformation of each centre to the combined IGL orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1472.0 GPS week: 1472 Day: 0 MJD: 54548
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 67| 1 -1 0 -92 -27 -52 -.18 30 30 | 0 45 2129 2187
cod 175| -2 2 1 60 9 41 -.19 27 19 | --- --- --- ---
esx 113| 0 0 -10 60 22 36 .58 77 43 | 29579 824 6059 25037
iac n/a| 2 0 -1 -91 -28 -69 .21 59 59 | 1201463 -3382 5657 18340
mcc n/a| 3 21 -28 -307 45 2054 -.21 363 363 | --- --- --- ---
Table 2.1472.1 GPS week: 1472 Day: 1 MJD: 54549
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 67| 2 0 -7 -65 -7 35 -.20 38 34 | 0 135 2255 2390
cod 175| -1 2 5 15 20 43 -.24 25 20 | --- --- --- ---
esx 113| 4 -2 -15 -78 15 -178 .74 91 70 | 17235 12241 10823 26750
iac n/a| 4 -1 -1 -13 -4 28 .19 55 55 | 1182587 4133 10516 17684
mcc n/a| 4 -14 47 187 -216 2051 -.14 334 334 | --- --- --- ---
Table 2.1472.2 GPS week: 1472 Day: 2 MJD: 54550
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 67| 3 -2 -5 -39 64 -44 -.13 34 33 | 0 29 2423 2518
cod 175| 1 0 0 16 17 -1 -.17 31 24 | --- --- --- ---
esx 113| -5 -7 -1 14 -117 66 .25 237 55 | -25337 -4281 7921 25701
iac n/a| 4 5 18 27 47 -98 .11 60 60 | 1137621 -6819 7636 18694
mcc n/a| -21 -10 60 264 416 2351 .64 217 217 | --- --- --- ---
Table 2.1472.3 GPS week: 1472 Day: 3 MJD: 54551
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 67| 8 0 -8 -32 28 -84 -.09 48 46 | 0 364 2504 2568
cod 175| 0 0 -2 46 11 80 -.19 26 23 | --- --- --- ---
esx 113| -3 -4 8 -30 -88 -82 .26 62 49 | 6449 4075 6048 22738
iac n/a| 2 0 3 -28 82 -15 .21 62 62 | 1161359 -724 5995 14365
mcc n/a| -29 29 24 -246 288 1946 .58 197 197 | --- --- --- ---
Table 2.1472.4 GPS week: 1472 Day: 4 MJD: 54552
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 67| 0 -2 0 -18 38 -95 -.10 44 37 | 0 -123 2599 2712
cod 175| 1 3 0 23 75 70 -.16 24 25 | --- --- --- ---
esx 113| 1 -8 -2 14 -131 101 .23 90 84 | 5169 5833 6461 20548
iac n/a| -1 1 -3 0 -57 -69 .22 53 53 | 1157727 -1315 6389 12595
mcc n/a| 1 -20 7 -513 85 904 -1.30 334 334 | --- --- --- ---
Table 2.1472.5 GPS week: 1472 Day: 5 MJD: 54553
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 67| -1 -1 0 -58 65 13 -.10 43 42 | 0 -365 3104 3189
cod 175| -3 -1 -2 69 -3 -4 -.16 23 17 | --- --- --- ---
esx 113| 12 -2 -2 6 22 6 .19 73 48 | -42643 -3243 7450 20838
iac n/a| -5 -2 5 -40 -33 -5 .24 44 44 | 1095475 -4540 7650 16452
mcc n/a| 0 2 82 296 -49 -724 1.29 180 180 | --- --- --- ---
Table 2.1472.6 GPS week: 1472 Day: 6 MJD: 54554
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 67| 0 -2 -5 -26 54 -511 -.13 42 37 | 0 262 2965 3051
cod 175| -1 0 -9 45 -67 185 -.08 24 22 | --- --- --- ---
esx 113| 3 5 3 -18 -71 64 .21 61 58 | -31439 -1037 7363 17093
iac n/a| 0 -1 13 -33 84 55 .09 39 39 | 1109661 -1994 7387 11423
mcc n/a| 2 9 24 177 22 -261 .37 358 358 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGL column gives resulting satellite accuracy measures found in
SP3 header. The last IGL column gives the RMS fit of the IGL orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGL orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.1472.0 GPS week: 1472 Day: 0 MJD: 54548
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 9610 29 14 27 49 --- 16 | 46 42 67 46 --- 44
R04 | 3548 18 11 41 31 --- 13 | 37 21 71 48 --- 28
R06 | 5082 32 15 39 38 --- 17 | 46 43 44 61 --- 39
R07 | 3224 18 19 30 39 99 14 | 33 31 38 58 178 33
R08 | 6151 26 14 105 64 --- 29 | 57 39 74 55 --- 33
R09 | 8788 43 24 181 29 --- 42 | 30 23 169 42 --- 34
R10 | 1685 29 18 55 40 --- 19 | 59 44 48 40 --- 43
R11 | 3731 18 30 55 65 --- 23 | 35 52 135 43 --- 39
R13 |11266 31 25 44 36 --- 18 | 32 54 59 53 --- 43
R14 | 1715 16 19 22 22 --- 11 | 34 48 46 28 --- 35
R15 | 2821 34 20 35 39 224 17 | 65 55 58 43 119 47
R17E |11344 44 59 120 135 --- 48 | 32 32 101 117 --- 39
R19E | 1757 36 27 42 98 --- 29 | 35 30 45 85 --- 28
R20E | 1665 29 25 61 60 --- 23 | 36 38 74 61 --- 37
R23E | 770 23 42 121 53 --- 33 | 41 58 111 76 --- 57
R24E | 4431 30 24 47 38 579 19 | 39 43 70 50 429 38
------+------------------------------------+--------------------------------
RMS | 5945 30 27 77 59 363 |T 41 40 75 56 242 38
WRMS | 5945 30 19 43 59 363 |NE 43 41 73 47 148 38
MEDI | 3548 29 20 44 39 224 |MD 36 42 67 50 178 38
Table 3.1472.1 GPS week: 1472 Day: 1 MJD: 54549
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |>>>>> 24 23 32 34 --- 15 | 43 56 56 56 --- 46
R04 |>>>>> 17 20 261 28 --- 15 | 24 23 158 43 --- 24
R06 |>>>>> 41 9 29 30 --- 16 | 32 32 53 39 --- 24
R07 |>>>>> 36 18 33 21 235 15 | 62 47 65 51 161 51
R08 |>>>>> 87 19 128 54 --- 40 | 71 29 111 44 --- 22
R09 |14038 21 18 54 21 --- 16 | 25 22 82 55 --- 31
R10 |>>>>> 38 13 54 19 --- 17 | 69 37 45 34 --- 40
R11 |>>>>> 32 36 90 44 --- 27 | 30 66 244 54 --- 40
R13 |16560 37 36 82 66 --- 29 | 27 69 78 78 --- 43
R14 |>>>>> 18 10 59 26 --- 16 | 30 40 88 24 --- 38
R15 |>>>>> 24 36 55 73 224 27 | 41 66 63 43 93 42
R17E |13920 24 25 67 84 --- 28 | 32 55 54 81 --- 44
R19E |>>>>> 48 35 69 111 --- 37 | 38 30 64 81 --- 31
R20E |>>>>> 40 26 82 68 --- 29 | 47 48 71 78 --- 39
R23E |>>>>> 37 34 37 55 --- 23 | 34 42 64 60 --- 31
R24E |>>>>> 29 24 46 40 479 19 | 19 25 59 47 461 24
------+------------------------------------+--------------------------------
RMS |>>>>> 38 25 91 55 334 |T 39 42 84 54 238 35
WRMS |>>>>> 34 20 70 55 334 |NE 41 44 94 47 127 36
MEDI |>>>>> 32 23 55 40 235 |MD 32 40 64 51 161 38
Table 3.1472.2 GPS week: 1472 Day: 2 MJD: 54550
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7159 23 24 60 57 --- 22 | 24 51 60 36 --- 33
R04 | 3232 40 20 46 49 --- 21 | 28 34 48 69 --- 37
R06 | 8021 19 15 43 57 --- 19 | 31 44 64 62 --- 41
R07 | 1146 22 16 29 46 207 16 | 33 31 37 60 111 30
R08 | 4981 52 35 99 23 --- 30 | 46 40 123 48 --- 46
R09 | 6130 36 28 127 57 --- 35 | 25 25 160 44 --- 32
R10 | 2411 36 16 43 27 --- 17 | 42 39 50 40 --- 32
R11 | 3963 35 53 914 92 --- 41 | 37 75 758 67 --- 43
R13 | 7129 19 26 69 45 --- 22 | 49 49 78 71 --- 47
R14 | 2748 19 19 59 35 --- 18 | 30 44 81 32 --- 35
R15 | 3139 42 21 60 43 199 23 | 53 51 92 61 56 48
R17E | 6528 47 49 53 70 --- 31 | 35 54 60 90 --- 30
R19E | 1085 26 49 47 115 --- 35 | 39 32 51 75 --- 28
R20E | 1488 40 27 66 78 --- 29 | 27 41 97 77 --- 42
R23E | 2211 20 35 71 53 --- 25 | 53 44 77 77 --- 45
R24E | 2118 34 20 31 49 242 19 | 27 33 49 58 253 30
------+------------------------------------+--------------------------------
RMS | 4575 34 31 237 60 217 |T 36 42 117 60 140 37
WRMS | 4575 33 24 55 60 217 |NE 36 43 141 53 83 38
MEDI | 3139 34 24 59 49 207 |MD 33 41 64 61 111 35
Table 3.1472.3 GPS week: 1472 Day: 3 MJD: 54551
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6193 40 24 37 32 --- 18 | 55 50 106 45 --- 45
R04 | 3173 23 18 30 30 --- 14 | 29 31 92 48 --- 32
R06 | 2776 56 26 41 39 --- 22 | 35 52 72 53 --- 47
R07 | 1644 33 14 49 50 269 20 | 36 47 56 57 129 40
R08 | 5309 83 28 117 45 --- 39 | 65 58 113 57 --- 42
R09 | 7831 66 24 81 48 --- 30 | 32 46 90 50 --- 39
R10 | 2521 49 27 33 38 --- 20 | 71 43 45 48 --- 44
R11 | 4688 36 48 93 98 --- 38 | 52 93 143 84 --- 65
R13 | 7825 23 26 58 61 --- 23 | 51 59 100 39 --- 51
R14 | 4926 32 14 23 24 --- 13 | 62 38 49 50 --- 43
R15 | 3503 74 13 69 61 145 30 | 79 65 94 73 37 55
R17E | 9335 51 27 75 43 --- 27 | 36 42 84 40 --- 39
R19E | 1327 35 33 54 112 --- 34 | 38 36 81 84 --- 41
R20E | 1500 31 30 50 88 --- 28 | 36 51 72 74 --- 41
R23E | 2198 47 24 65 91 --- 31 | 39 38 83 83 --- 41
R24E | 2414 43 20 41 37 151 19 | 41 35 64 52 214 39
------+------------------------------------+--------------------------------
RMS | 4849 48 26 62 62 197 |T 47 49 84 58 126 44
WRMS | 4849 46 23 49 62 197 |NE 51 52 87 54 83 45
MEDI | 3173 40 24 50 45 151 |MD 39 46 83 52 129 41
Table 3.1472.4 GPS week: 1472 Day: 4 MJD: 54552
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6638 23 20 273 28 --- 16 | 34 47 195 33 --- 32
R04 | 3568 22 11 31 17 --- 11 | 28 21 29 41 --- 18
R06 | 3126 70 26 35 25 --- 24 | 111 54 47 70 --- 64
R07 | 1457 30 20 35 43 486 17 | 37 27 40 62 249 32
R08 | 5166 57 22 66 33 --- 25 | 39 50 65 56 --- 39
R09 |17736 37 21 64 33 --- 21 | 31 36 60 43 --- 30
R10 | 2734 59 43 47 54 --- 28 | 63 45 42 39 --- 33
R11 | 5823 50 23 77 63 --- 29 | 60 60 96 80 --- 53
R13 | 7865 21 25 65 38 --- 21 | 69 45 89 52 --- 50
R14 | 2415 17 21 27 38 --- 14 | 36 21 37 22 --- 21
R15 | 8958 58 13 76 89 94 33 | 55 33 90 55 53 36
R17E | 8506 41 25 81 59 --- 28 | 44 45 84 47 --- 34
R19E | 1295 29 27 78 62 --- 27 | 30 53 87 54 --- 40
R20E | 3090 38 21 42 60 --- 22 | 35 49 76 70 --- 49
R23E | 1358 62 31 86 89 --- 36 | 41 37 99 97 --- 46
R24E | 1864 31 23 40 53 299 20 | 33 34 47 66 289 34
------+------------------------------------+--------------------------------
RMS | 6558 44 24 90 53 334 |T 46 41 73 55 197 38
WRMS | 6558 37 25 84 53 334 |NE 51 39 71 50 151 37
MEDI | 3126 37 22 64 43 299 |MD 37 45 65 54 249 34
Table 3.1472.5 GPS week: 1472 Day: 5 MJD: 54553
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6784 27 33 71 34 --- 23 | 35 32 69 47 --- 35
R04 | 3294 45 12 25 47 --- 18 | 44 24 60 42 --- 25
R06 | 5185 51 20 43 29 --- 19 | 76 50 59 70 --- 57
R07 | 3832 48 20 23 58 215 22 | 25 36 62 82 252 43
R08 | 4747 46 13 138 41 --- 34 | 58 60 97 64 --- 50
R09 |10477 26 9 22 28 --- 11 | 25 24 52 45 --- 23
R10 | 1398 50 15 24 32 --- 17 | 57 17 49 36 --- 25
R11 |11085 34 23 25 30 --- 16 | 24 52 67 34 --- 36
R13 |10352 48 28 180 47 --- 43 | 30 35 199 33 --- 38
R14 | 2755 38 23 29 50 --- 20 | 34 37 44 18 --- 25
R15 | 8786 33 29 57 28 86 20 | 42 44 66 40 54 32
R17E | 9859 42 36 68 67 --- 29 | 43 64 84 51 --- 44
R19E | 1521 27 18 54 29 --- 17 | 37 30 73 37 --- 28
R20E | 6196 46 21 73 40 --- 23 | 44 34 74 43 --- 35
R23E | 1922 66 25 58 71 --- 30 | 33 35 71 72 --- 34
R24E | 1843 39 19 69 50 210 23 | 58 49 89 80 144 58
------+------------------------------------+--------------------------------
RMS | 6579 43 23 73 44 180 |T 41 38 75 49 150 36
WRMS | 6579 42 17 48 44 180 |NE 40 37 74 46 153 35
MEDI | 4747 42 20 54 40 210 |MD 37 35 67 43 144 35
Table 3.1472.6 GPS week: 1472 Day: 6 MJD: 54554
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6403 19 23 43 22 --- 15 | 34 40 82 28 --- 30
R04 | 2862 32 25 37 17 --- 16 | 36 19 68 28 --- 21
R06 | 6553 27 17 38 20 --- 14 | 48 58 76 49 --- 47
R07 | 5827 19 19 48 21 179 14 | 36 32 48 48 145 27
R08 | 4758 76 28 119 34 --- 36 | 97 55 81 48 --- 60
R09 | 9533 28 25 52 49 --- 21 | 33 31 68 59 --- 31
R10 | 2424 40 19 79 37 --- 23 | 44 27 64 33 --- 24
R11 | 7964 27 27 106 27 --- 27 | 43 57 113 25 --- 30
R13 |14896 57 34 67 40 --- 27 | 124 64 69 96 --- 81
R14 | 2062 31 18 31 28 --- 15 | 45 39 51 25 --- 31
R15 | 5365 47 14 53 15 93 18 | 58 43 48 40 42 41
R17E |12371 64 21 37 55 --- 26 | 42 52 51 53 --- 40
R19E | 2354 28 21 45 29 --- 16 | 33 24 66 64 --- 32
R20E | 5187 31 24 29 37 --- 17 | 45 51 65 50 --- 41
R23E | 1657 57 34 74 88 --- 36 | 53 52 58 114 --- 55
R24E | 2089 29 21 33 45 586 18 | 45 52 60 54 182 46
------+------------------------------------+--------------------------------
RMS | 6876 42 24 61 39 358 |T 51 43 66 50 123 39
WRMS | 6876 37 22 58 39 358 |NE 54 42 69 43 93 38
MEDI | 5187 31 21 45 29 179 |MD 44 43 65 48 145 32
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